UAS OSC Volume 2

WARNING: This document was generated automatically and may contain errors and/or ommissions. You MUST review the data and satisfy yourself that it is complete and accurate. There is a link to the original source of the data below to help you do that.

Operator ID:
UAS Operating Safety Case Volume 2 - UAS Description:
Document reference number:
Document version and date:

Amendment record

Amendment Number	Date	Amended by	Details of changes

CAP722A Table 6

Aircraft and systems description

UAS Model	FPV
UAS design & manufaturing organisations	DJI

UAS physical characteristics

Empty Mass
Maximum Take-Off Mass (MTOM)	Takeoff Weight: Approx. 795 g
Dimensions for Rotorcraft / Multirotor
Length of aircraft body	Dimensions: 255 x 312 x 127 mm (with propellers) 178 x 232 x 127 mm (without propellers) Diagonal Distance: 245 mm
Width of aircraft body
Height of aircraft body
Propeller Configuration
Propeller Dimensions
Sound power level
Any other relevant information

CAP722A Table 7

UAS performance characteristics

Maximum airspeed	Max Speed (near sea level, no wind): 140 kph; M mode: 39 m/s (27 m/s in Mainland China) S mode: 27 m/s N mode: 15 m/s
Minimum airspeed to maintain safe flight
Normal/typical operating height
Maximum operating height	Max Service Ceiling Above Sea Level: 6,000 m
Maximum flight time during normal operation	Max Flight Time: Approx. 20 mins (measured while flying at 40 kph in windless conditions)
Maximum flight time on an ISA day at cruising speed at normal/typical operating height.
Maximum flight range on an ISA day (normal and emergency conditions)	Max Flight Distance: 16.8 km (measured while flying in windless conditions)
Glide distances
Maximum radio range of the C2 Link	Transmission Range [2]: 10 km (FCC), 6 km (CE), 6 km (SRRC), 6 km (MIC) Max. Transmission Distance: 10 km (FCC), 6 km (CE), 6 km (SRRC), 6 km (MIC) Max Transmission Distance (unobstructed, free of interference): 10 km (FCC), 6 km (CE/SRRC/MIC)

CAP722A Table 8

UAS environmental limitations

Wind speed limits	Max Wind Speed Resistance: 39-49 kph (25-31 mph)
Turbulence restrictions
Precipitation limits
OAT limits	Operating Temperature: -10 Deg. to 40 Deg. C (14 Deg. to 104 Deg. F)
In-flight icing condition limits
Any other relevant information

CAP722A Table 9

Construction

Type of material
Material characteristics or properties
Any other relevant information

CAP722A Table 10

Electrical power system

Batteries:
Battery type, model and manufacturer	Battery Type: LiPo 6S Battery Capacity: 2000 mAh
Quantity
Arrangement
Generator:
Generator type, model and manufacturer
Specification
Electrical loads	Voltage: 22.2 V Energy: 44.4 Wh@0.5C
Electrical load shedding functionality	Discharge Rate: Standard: 10C
Power supply redundancy
Procedures to charge and discharge batteries.
Safety provisions with regards to hazards inherent to high-voltage storage devices:
Procedures in place for safe handling by any person who may come into contact with high-voltage storage devices
Means of identifying high-voltage storage
Safety provisions for any person discovering the UA following an accident.
Procedures and safety provisions to mitigate the risk of battery thermal runaway.
Procedures for monitoring high-voltage storage devices.
HMI:
Information indicated to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information	Charging Temperature: 5 Deg. to 40 Deg. C (41 Deg. to 104 Deg. F)

CAP722A Table 11

Propulsion system

Propulsion type
Engines:
Type, model and manufacturer
Propeller type, model and manufacturer
Quantity
Arrangement
Power output
Propeller guards
In-flight restart functionality
Performance monitoring
Health monitoring
Safety features and redundancy in the system that allow maintaining flight after a failure or degradation has occurred in the propulsion system.
Fuel-powered propulsion system – Safety features to mitigate the risk of engine loss when the following hazards occur:
Fuel starvation
Fuel contamination
Failed signal input from the control station
Engine controller failure
Indication to the remote pilot
Electric-powered propulsion system:
Power source and supply management with regards to other systems in the UA
Redundant power sources
Maximum continuous power output of the motor
Maximum peak power output of the motor
Electrical distribution architecture
Electrical load shedding functionality
HMI:
Information indicated to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information

CAP722A Table 12

Fuel system

Fuel type
Safety provisions with regards to hazardous substances within the fuel system:
List of hazardous substances and their characteristics.
Procedures in place for safe handling of the UA by any person who may come into contact with the hazardous substances.
Means of identifying the hazardous substances.
Safety provisions for any person discovering the UA following an accident.
HMI:
Information indicated to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information

CAP722A Table 13

Flight Controls system

Design and operation of flight control units, surfaces, actuators, control linkages, etc.
Flight controller:
Type, model and manufacturer	Model: FC7BMC
Functions
Flight modes available
Automatic functions:
Take-off and landing
Stabilisation
Autopilot
Return to home
If functions are provided by COTS equipment, provide type, model and manufacturer.
Safety features and redundancy in the system which allow maintaining flight after a failure or degradation of the flight control system, including indication to the remote pilot.
HMI:
Information indicated to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information

CAP722A Table 14

Navigation

Sensors
Type, model and manufacturer	GNSS: GPS+GLONASS+GALILEO
Quantity
Telemetry links
Method to determine current position.
Method to navigate to intended destination.
Automatic/automated navigation functions
Geo-awareness functions
Containment functions
Safety features and redundancy in the system which allow maintaining flight after a failure or degradation has occurred in the navigation system:
Backup means of navigation
Detection of and response to loss of primary means and secondary means of navigation.
Indication to the remote pilot
HMI:
Information indicated to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information

CAP722A Table 15

Detect and Avoid (DAA) systems

DAA system functions	Forward: Precision Measurement Range: 0.5-18 m Obstacle Sensing: Available in N mode only FOV: 56 Deg. (horizontal), 71 Deg. (vertical) Downward: ToF Effective Sensing Height: 10 m Hovering Range: 0.5-15 m Vision Sensor Hovering Range: 0.5-30 m Operating Environment: Refers to non-reflective, discernible surfaces Diffuse reflectivity >20% (e.g. walls, trees, people) Adequate lighting conditions (lux >15 in normal indoor lighting conditions)
Devices used
Technology used
Interface between the DAA system and the flight control computer
Limitations of the DAA system
Evidence of equipment qualification and approval.
DAA event sequence:
Level of automation
Actions required by the remote pilot
Means to verify normal system operation.
HMI:
Information indicated to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information

CAP722A Table 16

Other avionics systems

Command Unit (CU)

Power sources, supply management and redundancy.
Radio signal:
Determination of the signal strength and health value.
Threshold values which represent a critically degraded signal.
Control handover between two CUs
Safety features to mitigate the risk of inadvertent command activation:
List of critical commands
Mitigation means
Safety features to mitigate the risk of display or HMI lock-up.
Safety features to maintain flight-critical processing when multiple programs are running concurrently.
HMI:
Information indicated to the remote pilot.
Radio signal strength and/or health indication to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information	Battery Life: Approx. 9 hours Weight: 346 g Battery Life: 300 minutes Operating Temperature Range: -10 Deg. to 40 Deg. C (14 Deg. to 104 Deg. F)

CAP722A Table 17

Command an Control (C2) link

RLOS
BRLOS
Antennas:
Type, model and manufacturer	Number of Antennas: Four
Locations on the UAS
Transceivers / Modems:
Power levels	Transmitter Power (EIRP): 2.400-2.4835 GHz FCC: <= 31.5dBm CE: <= 20 dBm SRRC: <= 20 dBm MIC: <= 20 dBm 5.725-5.850 Ghz FCC: <= 31.5 dBm CE: <= 14 dBm SRRC: <= 25.5 dBm Transmitter Power (EIRP): 2.400-2.4835 GHz FCC: <= 28.5 dBm CE: <= 20 dBm SRRC: <= 20 dBm MIC: <= 20 dBm 5.725-5.850 GHz FCC: <= 31.5 dBm CE: <= 14 dBm SRRC: <= 19 dBm Transmitter Power (EIRP): 2.400-2.4835 GHz FCC: <= 28.5 dBm CE: <= 20 dBm SRRC: <= 20 dBm MIC: <= 20 dBm 5.725-5.850 GHz FCC: <= 31.5 dBm CE: <= 14 dBm SRRC: <= 19 dBm Transmitter Power (EIRP): 2.4 GHz: <=28.5 dBm (FCC), <=20 dBm (CE/ SRRC/MIC) 5.8 GHz: <=31.5 dBm (FCC), <=19 dBm (SRRC), <=14 dBm (CE)
Transmission schemes
Operating frequencies
Details of frequency spectrum approvals	Operating Frequency: 2.400-2.4835 GHz 5.725-5.850 GHz Operating Frequency Range: 2.400-2.4835 GHz; 5.725-5.850 GHz
Maximum power output/range
Type of signal processing
Datalink margin in terms of the overall link bandwidth at the maximum anticipated distance from the CU.
Operational C2 link management:
Frequency switchovers
Contingency situations
Third party link service provider
Radio signal:
Determination of the signal strength and health value
Threshold values which represent a critically degraded signal.
Minimum and average assured data rates
Minimum and average assured latencies
Design features and procedures to maintain availability, continuity, and integrity of the datalink:
RF or other interference
Flight beyond communications range
Antenna masking
Loss of CU functionality
Loss of UA functionality
Atmospheric attenuation
Safety features to mitigate the risk of loss of C2 link:
C2 links redundancy
Automatic triggering of an emergency recovery function
Automatic return to home
Safety features to mitigate the risk of harmful interference.
HMI:
Information indicated to the remote pilot.
Radio signal strength and/or health indication to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information

CAP722A Table 18

Communications

Antennas:
Type, model and manufacturer
Locations on the UAS
Communication method:
VHF
GSM network
Satellite
Safety features to mitigate the loss of communication function:
Primary communication means
Secondary / back-up communication means
HMI:
Information indicated to the remote pilot.
Radio signal strength and/or health indication to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information

CAP722A Table 19

Take-off and landing mechanisms

Wheels, skids, rails, launchers, etc.
If various mechanisms can be fitted:
Primary mechanism
Secondary mechanisms
Operational conditions/requirements for each mechanism.
Any other relevant information

CAP722A Table 20

Emergency recovery and safety systems

Mode of operation
Safety features which mitigate the risk of loss of control or situational awareness.
Means to verify normal system operation.
HMI:
Information indicated to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information

CAP722A Table 21

External lighting

Type, model and manufacturer	Downward Auxillary Light: Single LED
Locations on the UA
Colour
Operation
Operating modes
Purpose
HMI:
Information indicated to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information

CAP722A Table 22

Payload

Types
Mass
Interfaces with the UA:
Mechanical interface
Electrical interface
Data interface
Release mechanism
Any other interface
Procedures to install the payload onto the UA.
Effects of the payload on the UA
Sensors	Sensor: 1/2.3" CMOS Effective pixels: 12 million
Safety features to mitigate the risk of the payload affecting the flight of the UA:
Effects on aerodynamics
Effects of electro-magnetic interference.
Effects of electrical power and / or data connection failures on the UAS.
Effects of complete detachment of the payload from the UA (either caused by a failure or through intentional lowering / dropping of the payload).
Effects of partial detachment of the payload from the UA.
Distraction of the remote pilot generated by the payload during flight.
Procedures to verify the attachment points to the UA.
Procedures to verify the UA MTOM and CG location.
Procedures to detect and mitigate any failure of the payload in flight.
Safety provisions with regards to hazards inherent to the payload
Procedures in place for safe handling of the payload.
Means of identifying hazards.
HMI:
Information indicated to the remote pilot.
Alert messages indicated to the remote pilot.
Any other relevant information

CAP722A Table 23

Ground support equipment

UAS launch and recovery systems
Power sources
Transportation equipment
Backup or emergency equipment
Procedures to transport UA, CU, battery/fuel, and other equipment between operation sites and from the loading/off-loading area to the take-off/landing area.
Storage of ground support equipment.
Suitability of the ground support equipment and transportation method with regards to the UAS components’ fragility, sensitivity or inherent hazards.
Ground support equipment standards
Ground support equipment manufacturer's recommendations.
Any other relevant information

CAP722A Table 24

Maintenance

Maintenance manual:
Structure
Maintenance procedures:
Inspections
Overhaul
Repairs
Assurance of repair procedures
Batteries maintenance during storage periods
Origin of each procedure
Maintenance schedules
Procedures to record maintenance that has been carried out.
Storage of maintenance records
Staff qualification and levels of approval.
Procedures to use the manual by the Maintenance staff
Configuration control
Any other relevant information

CAP722A Table 25

Spare parts procurement

Sources of procurement
Process to confirm the suitability of the part.
Any other relevant information

CAP722A Table 26

Change Management and modifications to the system

Hardware, software, and firmware version control
Modification standards
Modification records storage
Safety assessment associated with the modification
Any other relevant information

CAP722A Table 27

Safety features of the UAS

Step 1 – Identify the main functions of the UAS.
Step 2 – Identify the sub-functions.
Step 3 – Consider the ways each function may fail.
Step 4 – Identify the failure conditions.
Step 5 – Select those failure conditions that may lead to mid-air collision or harm to uninvolved people on the ground. (Identified Hazard)
Step 6 – Assurance
Step 7 – Describe the consequence of the failure condition.
Step 8 – Describe the failure modes. (Unmitigated Failures)
Step 9 – Identify the single points of failure.
Step 10 – Describe the risk mitigation means.

CAP722A Table 28

ANNEX - Manufacturer supplied data forDJI FPV

Camera
Sensor	1/2.3" CMOS Effective pixels: 12 million
Lens	FOV: 150 Deg. 35mm Format Equivalent: 14.66 mm Aperture: f/2.8 Focus Mode: Fixed Focus Focus Range: 0.6 m to ∞
ISO	100-12800
Shutter Speed	1/50-1/8000 s
Still Photography Modes	Single shot
Max Image Size	3840 x 2160
Photo Format	JPEG
Video Resolution	4K: 3840 x 2160 at 50/60fps FHD: 1920 x 1080 at 50/60/100/120fps
Video Formats	MP4/MOV (H.264/MPEG-4 AVC, H.265/HEVC)
Max Video Bitrate	120 Mbps
Color Profile	Standard, D-Cinelike
RockSteady EIS	Available
Distortion Correction	Available
Supported File Formats	exFAT (recommended) FAT32
Gimbal
Mechanical Range	Tilt: -65 Deg. to 70 Deg.
Controllable Range	Tilt: -50 Deg. to 58 Deg.
Stabilization	Single-axis (tilt), electronic roll axis
Max Control Speed (tilt)	60 Deg./s
Angular Vibration Range	±0.01 Deg. (N mode)
Electronic Roll Axis	Available (can stabilize footage when the aircraft is tilted at angles of up to 10 Deg.)
Aircraft
Takeoff Weight	Approx. 795 g
Dimensions	255 x 312 x 127 mm (with propellers) 178 x 232 x 127 mm (without propellers)
Diagonal Distance	245 mm
Max Ascent Speed	M mode: No limit S mode: 15 m/s N mode: 8 m/s
Max Descent Speed	M mode: No limit S mode: 10 m/s N mode: 7 m/s
Max Speed (near sea level, no wind)	140 kph; M mode: 39 m/s (27 m/s in Mainland China) S mode: 27 m/s N mode: 15 m/s
Max Acceleration	0-100 kph: 2 s (in ideal conditions while flying in M mode)
Max Service Ceiling Above Sea Level	6,000 m
Max Flight Time	Approx. 20 mins (measured while flying at 40 kph in windless conditions)
Max Hover Time (without wind)	Approx. 16 mins (measured when flying in windless conditions)
Max Flight Distance	16.8 km (measured while flying in windless conditions)
Max Wind Speed Resistance	39-49 kph (25-31 mph)
Operating Temperature	-10 Deg. to 40 Deg. C (14 Deg. to 104 Deg. F)
Transmitter Power (EIRP)	2.400-2.4835 GHz FCC: <= 31.5dBm CE: <= 20 dBm SRRC: <= 20 dBm MIC: <= 20 dBm 5.725-5.850 Ghz FCC: <= 31.5 dBm CE: <= 14 dBm SRRC: <= 25.5 dBm
Number of Antennas	Four
GNSS	GPS+GLONASS+GALILEO
Hovering Accuracy Range	Vertical: ±0.1 m (with Vision Positioning) ±0.5 m (with GPS positioning) Horizontal: ±0.3 m (with Vision Positioning) ±1.5 m (with GPS positioning)
Supported SD Cards	microSD (up to 256 GB)
Internal Storage	N/A
Sensing System
Forward	Precision Measurement Range: 0.5-18 m Obstacle Sensing: Available in N mode only FOV: 56 Deg. (horizontal), 71 Deg. (vertical)
Downward	ToF Effective Sensing Height: 10 m Hovering Range: 0.5-15 m Vision Sensor Hovering Range: 0.5-30 m
Downward Auxillary Light	Single LED
Operating Environment	Refers to non-reflective, discernible surfaces Diffuse reflectivity >20% (e.g. walls, trees, people) Adequate lighting conditions (lux >15 in normal indoor lighting conditions)
Charger
Input	100-240 V, 50/60 Hz, 1.8 A
Output	Battery charging interface: 25.2 V ± 0.1 V 3.57 A ± 0.1 A (high current) 1 A ± 0.2 A (low current) USB Port: 5V/2A ( x 2)
Rated Power	86 W
Intelligent Flight Battery
Battery Capacity	2000 mAh
Voltage	22.2 V
Max Charging Voltage	25.2 V
Battery Type	LiPo 6S
Energy	44.4 Wh@0.5C
Discharge Rate	Standard: 10C
Weight	295 g
Charging Temperature	5 Deg. to 40 Deg. C (41 Deg. to 104 Deg. F)
Max Charging Power	90 W
Video Transmission
Operating Frequency	2.400-2.4835 GHz 5.725-5.850 GHz
Communication Bandwidth	40 MHz (Max.)
Live View Mode	Low-Latency Mode: 810p/120fps <= 28ms High-Quality Mode: 810p/60fps <= 40ms
Max Video Bitrate	50 Mbps
Transmission Range	10 km (FCC), 6 km (CE), 6 km (SRRC), 6 km (MIC)
Audio Transmission Support	Yes
DJI FPV Goggles V2
Weight	Approx. 420 g (headband and antennas included)
Dimensions (L×W×H)	184 x 122 x 110 mm (antennas excluded) 202 x 126 x 110 mm (antennas included)
Screen Size (single screen)	2-inches ( x 2)
Screen Refresh Rate	144 Hz
Communication Frequency	2.400-2.4835 GHz 5.725-5.850 GHz
Transmitter Power (EIRP)	2.400-2.4835 GHz FCC: <= 28.5 dBm CE: <= 20 dBm SRRC: <= 20 dBm MIC: <= 20 dBm 5.725-5.850 GHz FCC: <= 31.5 dBm CE: <= 14 dBm SRRC: <= 19 dBm
Communication Bandwidth	40 MHz (Max.)
Live View Mode	Low-Latency Mode: 810p/120fps <= 28ms* High-Quality Mode: 810p/60fps <= 40ms* * A 150 Deg. FOV is available when shooting at 50 or 100 fps. For other frame rates, the FOV will be 142 Deg..
Max Video Bitrate	50 Mbps
Transmission Range [2]	10 km (FCC), 6 km (CE), 6 km (SRRC), 6 km (MIC)
Video Format	MOV(Video format: H.264)
Supported Video and Audio Playback Formats	MP4, MOV, MKV (Video format: H.264; Audio format: AAC-LC, AAC-HE, AC-3, MP3)
Operating Temperature	0 Deg. to 40 Deg. C (32 Deg. to 104 Deg. F)
Power Input	Dedicated DJI Goggles batteries
FOV	FOV: 30 Deg. to 54 Deg.; Image size: 50-100%
Interpupillary Distance Range	58-70 mm
Supported microSD Cards	microSD (up to 256 GB)
DJI FPV Goggles Battery
Capacity	1800 mAh
Voltage	9 V (Max.)
Type	LiPo 2S
Energy	18 Wh
Charging Temperature	0 Deg. to 45 Deg. C (32 Deg. to 113 Deg. F)
Max Charging Power	10 W
Battery Life	Approx. 110 minutes (measured in an environment of 25 Deg.C at maximum brightness level)
DJI FPV Remote Controller 2
Operating Frequency	2.400-2.4835 GHz 5.725-5.850 GHz
Transmitter Power (EIRP)	2.400-2.4835 GHz FCC: <= 28.5 dBm CE: <= 20 dBm SRRC: <= 20 dBm MIC: <= 20 dBm 5.725-5.850 GHz FCC: <= 31.5 dBm CE: <= 14 dBm SRRC: <= 19 dBm
Max. Transmission Distance	10 km (FCC), 6 km (CE), 6 km (SRRC), 6 km (MIC)
Dimensions (L×W×H)	190 x 140 x 51 mm
Weight	346 g
Battery Life	Approx. 9 hours
Charging Time	2.5 hours
Motion Controller
Model	FC7BMC
Weight	167 g
Operating Frequency Range	2.400-2.4835 GHz; 5.725-5.850 GHz
Max Transmission Distance (unobstructed, free of interference)	10 km (FCC), 6 km (CE/SRRC/MIC)
Transmitter Power (EIRP)	2.4 GHz: <=28.5 dBm (FCC), <=20 dBm (CE/ SRRC/MIC) 5.8 GHz: <=31.5 dBm (FCC), <=19 dBm (SRRC), <=14 dBm (CE)
Operating Temperature Range	-10 Deg. to 40 Deg. C (14 Deg. to 104 Deg. F)
Battery Life	300 minutes
microSD card
Supported microSD cards	Max 256 GBUHS-I Speed Grade 3
Recommended microSD cards	SanDisk High Endurance U3 V30 64GB microSDXC SanDisk Extreme PRO U3 V30 A2 64GB microSDXC SanDisk Extreme U3 V30 A2 64GB microSDXC SanDisk Extreme U3 V30 A2 128GB microSDXC SanDisk Extreme U3 V30 A2 256GB microSDXC Lexar 667x V30 128GB microSDXC Lexar High Endurance 128GB U3 V30 microSDXC Samsung EVO U3 (Yellow) 64GB microSDXC Samsung EVO Plus U3 (Red) 64GB microSDXC Samsung EVO Plus U3 256GB microSDXC Netac 256GB U3 A1 microSDXC
Footnotes:
Footnotes	1. Due to local policy and regulation restrictions, the 5.8 GHz frequency band is currently banned in certain countries, including but not limited to Japan, Russia, Israel, Ukraine, and Kazakhstan. Please use the 2.4 GHz frequency band when operating in these locations. Always check local rules and regulations before use, as they may change over time. 2. Maximum flight range specification is a proxy for radio link strength and resilience, not aircraft battery capability. It only refers to the maximum, one-way flight distance. Data was measured in an open environment without interference. Please pay attention to the return prompt on the DJI Fly app during actual flight. Refer to the following applicable standard in different countries and regions: FCC: United States, Australia, Canada, Hong Kong, Taiwan, Chile, Colombia, Puerto Rico, and other regions; SRRC: Mainland China; CE: UK, Russia, France, Germany, Portugal, Spain, Switzerland, Macau, New Zealand, UAE, and other regions; MIC: Japan.

Data source: https://www.dji.com/dji-fpv/specs

Generated using dronespec.info
Source data acquired 2023-01-23 19:03:42

UAS OSC Volume 2

WARNING: This document was generated automatically and may contain errors and/or ommissions. You MUST review the data and satisfy yourself that it is complete and accurate. There is a link to the original source of the data below to help you do that.

Amendment record

Aircraft and systems description

UAS physical characteristics

UAS performance characteristics

UAS environmental limitations

Construction

Electrical power system

Propulsion system

Fuel system

Flight Controls system

Navigation

Detect and Avoid (DAA) systems

Other avionics systems

Command Unit (CU)

Command an Control (C2) link

Communications

Take-off and landing mechanisms

Emergency recovery and safety systems

External lighting

Payload

Ground support equipment

Maintenance

Spare parts procurement

Change Management and modifications to the system

Safety features of the UAS

ANNEX - Manufacturer supplied data forDJI FPV

Camera

Gimbal

Aircraft

Sensing System

Charger

Intelligent Flight Battery

Video Transmission

DJI FPV Goggles V2

DJI FPV Goggles Battery

DJI FPV Remote Controller 2

Motion Controller

microSD card

Footnotes: